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d. Landing Configuration .......................................... FLAPS 50%
e. Airspeed ................................................................ 85-90 KIAS
Original Issue: 01-20-09
P/N 11934-S43 11 of 14
Cirrus Design Section 9
SR20 Supplements
Section 4 - Normal Procedures
Before Starting Engine
1. Preflight Inspection ...................................................COMPLETED
• WARNING •
Ensure that the airplane is properly loaded and within the
AFM’s weight and balance limitations prior to takeoff.
2. Weight and Balance............................................Verify within limits
3. Emergency Equipment ................................................ON BOARD
4. Passengers ..................................................................... BRIEFED
• Note •
Ensure all the passengers have been fully briefed on smoking,
the use of the seat belts, doors, emergency exits, egress
hammer, and CAPS.
Additionally, ensure all passengers have been briefed not to
touch and/or obstruct the control yokes or rudder pedals. The
pilot will demonstrate the full-extension of the controls so that
the passenger will understand needed clearances.
Verify CAPS handle safety pin is removed.
5. Passenger Door ..............................................................LATCHED
• Note •
From outside of aircraft verify both top and bottom latch of
door is securely latched. Press firmly at each door latch
position to ensure the security of door.
6. Seats, Seat Belts, and Harnesses ................ADJUST & SECURE
• Caution •
Crew seats must be locked in position and control handles
fully down before flight. Ensure seat belt harnesses are not
twisted.
Original Issue: 01-20-09
12 of 14 P/N 11934-S43
Section 9 Cirrus Design
Supplements SR20
Section 5 - Performance Data
Length Conversion
Meters Feet
200 656
400 1312
600 1969
800 2625
1000 3281
1200 3937
1400 4593
1600 5249
1800 5906
2000 6562
2200 7218
2400 7874
2600 8530
2800 9186
3000 9843
3200 10499
3400 11155
3600 11811
3800 12467
4000 13123
4200 13780
Original Issue: 01-20-09
P/N 11934-S43 13 of 14
Cirrus Design Section 9
SR20 Supplements
Section 6 – Weight and Balance
No Change.
Section 7 – Airplane and Systems Description
No Change.
Section 8 – Handling, Service, & Maintenance
No Change.
Section 9 – Supplements
No Change.
Section 10 – Safety Information
No Change.
Original Issue: 01-20-09
14 of 14 P/N 11934-S43
Section 9 Cirrus Design
Supplements SR20
Original Issue: 01-20-09
Intentionally Left Blank
P/N 13772-102 1 of 8
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
Garmin GTX 327 Transponder
When a Garmin GTX 327 Transponder is installed in the Cirrus Design
SR22, this Supplement is applicable and must be inserted in the
Supplements Section (Section 9) of the Cirrus Design SR22 Pilot’s
Operating Handbook. This document must be carried in the airplane at
all times. Information in this supplement adds to, supersedes, or
deletes information in the basic SR22 Pilot’s Operating Handbook.
Original: 12-12-00
2 of 8 P/N 13772-102
Section 9 Cirrus Design
Supplements SR22
Section 1 - General
The airplane is equipped with a single Garmin GTX 327 ATC Mode A/
C (identification and altitude) transponder with squawk capability. This
supplement provides complete operating instructions for the GTX 327
and does not require any additional data be carried in the airplane.
SR22_FM09_1501
1 2 3 4 5
10 9 8 7 6
1. Identification Key
2. Mode Selector Keys
a. OFF
b. STBY (Standby)
c. ON
d. ALT
3. Display Window
4. FUNC (Function) Key
5. CRSR (Cursor)
6. CLR (Clear) Key
7. START/STOP Key
8. Photocell
9. VFR Key
10. Selector Keys
a. 0-7 - Code Selection
b. 8-9 - Display Brightness/Contrast
Original: 12-12-00
P/N 13772-102 3 of 8
Cirrus Design Section 9
SR22 Supplements
Section 2 - Limitations
No Change
Section 3 - Emergency Procedures
No Change
Section 4 - Normal Procedures
• Note •
Expected coverage from the GTX 327 is limited to “line of
sight.” Low altitude or aircraft antenna shielding by the
　
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